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    COUPLING FOR CONNECTING AIR CIRCUIT PORTIONS OF AVIONICS RACK
    1.
    发明申请
    COUPLING FOR CONNECTING AIR CIRCUIT PORTIONS OF AVIONICS RACK 审中-公开

    公开(公告)号：US20190389584A1

    公开(公告)日：2019-12-26

    申请号：US16444419

    申请日：2019-06-18

    Applicant: AIRBUS OPERATIONS (S.A.S.)

    Inventor： Laurent SAINT-MARC ,  Bernard GUERING

    IPC: B64D13/06 ,  F02C7/04 ,  B64D33/02

    Abstract: A coupling is disclosed providing fluidic continuity between first and second orifices of two portions of an air circuit which includes a flexible sleeve, a first frame connected in fluid-tight manner to a first end of the flexible sleeve and having a first opening, and a second frame, connected in fluid-tight manner to a second end of the flexible sleeve and having a second opening. The coupling is deformable so that the flexible sleeve may adapt to the variable spacing between two avionics racks and is able to compensate for a misalignment between the orifices of two portions of an air circuit.

    AIRCRAFT ELECTRICAL CORE
    2.
    发明申请
    AIRCRAFT ELECTRICAL CORE 有权
    飞机电芯

    公开(公告)号：US20140209742A1

    公开(公告)日：2014-07-31

    申请号：US14227265

    申请日：2014-03-27

    Applicant: AIRBUS OPERATIONS S.A.S.

    Inventor： Bernard GUERING ,  Yves DURAND

    IPC: H05K7/02 ,  B64D47/00

    CPC classification number: H05K7/02 ,  B64D47/00 ,  H05K7/1439 ,  H05K7/1449

    Abstract: An electrical core of an aircraft is provided. The electrical core includes at least one shelf on which is disposed at least one module containing components and comprising at least one input able to be linked to at least one power supply cable and at least one output able to be linked to at least one output cable. In the module, the output cable or cables travel under or in the shelf disposed under the module.

    Abstract translation: 提供飞机的电芯。 电芯包括至少一个搁架，其上布置有至少一个包含部件的模块，并且包括至少一个能够连接到至少一个电源电缆的输入端和至少一个可连接到至少一个输出电缆 。 在模块中，输出电缆或电缆在设置在模块下方的架子下方或下方。

    METHOD FOR ALIGNING A FIRST HOLE OF A FIRST PART WITH A SECOND HOLE OF A SECOND PART AND KIT FOR ITS IMPLEMENTATION
    3.
    发明申请
    METHOD FOR ALIGNING A FIRST HOLE OF A FIRST PART WITH A SECOND HOLE OF A SECOND PART AND KIT FOR ITS IMPLEMENTATION 审中-公开

    公开(公告)号：US20170182643A1

    公开(公告)日：2017-06-29

    申请号：US15388800

    申请日：2016-12-22

    Applicant: AIRBUS OPERATIONS (S.A.S.)

    Inventor： Bernard GUERING

    IPC: B25B31/00 ,  B60B29/00 ,  F16B19/02 ,  B25B27/00

    Abstract: A method enabling two holes belonging to two parts to be aligned relies on use of a tool, comprising a body, having a first outer surface which gradually wanders from a longitudinal axis of the body as it extends from a first end of the body, and a hollow part having a second outer surface with a complementary section to the section of the holes. The hollow part comprises a hole through which it is removably mounted on the tool so that the second outer surface extends the first outer surface on an opposite side to the first end of the body. The method comprises inserting the first end of the body into the first hole, and then operating the tool to push the body and then the hollow part together into the holes. This method especially applies to the assembly of a floor module to an aircraft fuselage.

    METHOD AND DEVICE FOR FITTING OUT AN AIRCRAFT NOSE COMPARTMENT IN AN AVIONICS BAY
    4.
    发明申请
    METHOD AND DEVICE FOR FITTING OUT AN AIRCRAFT NOSE COMPARTMENT IN AN AVIONICS BAY 审中-公开
    用于在航空航天飞机上配备航空号码台的方法和装置

    公开(公告)号：US20130228655A1

    公开(公告)日：2013-09-05

    申请号：US13750115

    申请日：2013-01-25

    Applicant: AIRBUS OPERATIONS (S.A.S.)

    Inventor： Samuel BURGUNDER ,  Bernard GUERING

    IPC: B64C9/24 ,  B64C9/14

    CPC classification number: B64D11/00 ,  B64C1/061 ,  B64C1/20 ,  B64C9/14 ,  B64C9/24 ,  B64C25/02 ,  Y02T50/46

    Abstract: An aerodynamic body, with at least one ancillary flap arranged such that it can be moved on the aerodynamic body with the aid of a guide mechanism, and with a drive device for purposes of actuating the ancillary flap, the guide mechanism having a pivotal articulation, by which the ancillary flap is articulated on the aerodynamic body such that it can be extended, and which is arranged in a rear region of the ancillary flap as viewed in the flow direction.

    Abstract translation: 具有至少一个辅助翼片的空气动力学主体，其布置成使得其可以借助于引导机构而在空气动力学主体上移动，并且具有用于致动辅助翼片的驱动装置，所述引导机构具有枢转关节， 辅助翼片通过其铰接在空气动力体上，使得其可以延伸，并且布置在沿流动方向观察的辅助翼片的后部区域中。

    LINKING PART DESIGNED TO BE LINKED TO A SUPPORT ELEMENT OF AN AIRCRAFT
    5.
    发明申请
    LINKING PART DESIGNED TO BE LINKED TO A SUPPORT ELEMENT OF AN AIRCRAFT 审中-公开

    公开(公告)号：US20200172221A1

    公开(公告)日：2020-06-04

    申请号：US16698053

    申请日：2019-11-27

    Applicant: AIRBUS OPERATIONS (S.A.S.)

    Inventor： Bernard GUERING

    IPC: B64C1/06 ,  B64F5/10

    Abstract: A linking part for an aircraft is disclosed having an elongated section including an internal longitudinal seat and a tenon mounted in the seat. The tenon includes a linking element at a free longitudinal end thereof and configured in a retracted position in which the tenon is fully inserted in the seat and does not create an obstruction, enabling the linking part to be easily moved towards the support element, or a deployed position (P2) in which the free longitudinal end of the tenon is outside the seat and is able to be linked using the linking element to the support element, thereby enabling a link to be made simply and quickly.

    SEALED BOTTOM OF A FRONT END OF AN AIRCRAFT
    6.
    发明申请
    SEALED BOTTOM OF A FRONT END OF AN AIRCRAFT 审中-公开

    公开(公告)号：US20190185135A1

    公开(公告)日：2019-06-20

    申请号：US16225519

    申请日：2018-12-19

    Applicant: AIRBUS OPERATIONS (S.A.S.)

    Inventor： Bernard GUERING ,  Laurent SAINT-MARC

    IPC: B64C1/36 ,  B64C1/06

    CPC classification number: B64C1/36 ,  B64C1/06 ,  B64C1/061 ,  B64C1/068 ,  B64C1/10 ,  B64C2001/0045

    Abstract: A sealed bottom in the frame of a cockpit with centered pilot is disclosed for increasing the bulk inside the radome and making it possible to improve the optimization of the volumes. The sealed bottom includes a semi-cylindrical central part having four edges that are parallel in pairs, two curved edges, and two straight edges and a planar peripheral part extending at least partially around the central part. The peripheral part (22) is located in the plane of the straight edges of the central part and linked thereto. This configuration will allow to free up space to increase the number of passengers or reduce the size of the aircraft.

    REAR PRESSURE BULKHEAD WITH COMPOSITE-GEOMETRY INTEGRAL MEMBRANE
    7.
    发明申请
    REAR PRESSURE BULKHEAD WITH COMPOSITE-GEOMETRY INTEGRAL MEMBRANE 审中-公开

    公开(公告)号：US20180370611A1

    公开(公告)日：2018-12-27

    申请号：US16015409

    申请日：2018-06-22

    Applicant: AIRBUS OPERATIONS (S.A.S.)

    Inventor： Bernard GUERING ,  Laurent SAINT-MARC

    IPC: B64C1/10 ,  B64C1/06 ,  B64C1/18

    Abstract: A rear pressure bulkhead for aircraft with a semi-recessed integrated engine or, for aircraft of which the cross section of the tail cone in the region of the pressure bulkhead is of the ovoid type with inwardly curving side walls is provided. The cross section of the tail cone of such aircraft is atypical and subjected to loadings that make the application of a known shape of pressure bulkhead unsuitable. The integral membrane of which the geometric shape includes the combination of two substantially spherical half-caps and of a portion of a cylinder of substantially circular cross section joining the two half-caps, the free edges of the cylinder portion being slightly inwardly curved. Such a geometry allows the pressure bulkhead to withstand the loadings present in this zone.

    AIRCRAFT CONTROL COMPRISING AN IMPROVED PEDAL
    8.
    发明申请
    AIRCRAFT CONTROL COMPRISING AN IMPROVED PEDAL 审中-公开

    公开(公告)号：US20170283037A1

    公开(公告)日：2017-10-05

    申请号：US15471450

    申请日：2017-03-28

    Applicant: AIRBUS OPERATIONS (S.A.S.)

    Inventor： Bernard GUERING ,  Matthieu DE KERGOMMEAUX

    IPC: B64C13/04 ,  B64D13/08

    Abstract: An aircraft control of the rudder bar type, which includes a box-shaped pedal, a support, a first rotation shaft connecting the pedal to the support with a first rotation axis, a first pivot connection configured to allow the pedal to pivot about the first rotation axis relative to the support, a rod, a second rotation shaft, distinct from the first rotation shaft and connecting the pedal to the rod with a second rotation axis, and a second pivot connection configured so as to allow the pedal and/or the rod to pivot about the second rotation axis.

    AIRCRAFT PORTION COMPRISING A SUSPENDED ITEM OF FURNITURE EQUIPMENT
    9.
    发明申请
    AIRCRAFT PORTION COMPRISING A SUSPENDED ITEM OF FURNITURE EQUIPMENT 审中-公开

    公开(公告)号：US20200180768A1

    公开(公告)日：2020-06-11

    申请号：US16703733

    申请日：2019-12-04

    Applicant: AIRBUS OPERATIONS (S.A.S.)

    Inventor： Laurent SAINT-MARC ,  Bernard GUERING

    IPC: B64D11/04

    Abstract: An aircraft portion having a floor and a fuselage structure forming an arch above the floor is disclosed in which a monument is mounted within the fuselage. The monument is suspended from the fuselage structure by at least one suspension point, so that most of the weight of the monument is taken up by the fuselage structure. The monument includes a circular or a round section configured to take up the vertical forces than the horizontal floor, which bends under vertical loads.

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